View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 1577U 65065J 24358.15818000 .00000156 00000-0 28265-3 0 9995
2 1577 89.9963 211.2264 0069863 188.9846 295.6229 13.36121422890805
| Epoch (UTC): | 23 December 2024 03:47:46 |
| Eccentricity: | 0.0069863 |
| inclination: | 89.9963° |
| perigee height: | 1071 km |
| apogee height: | 1176 km |
| right ascension of ascending node: | 211.2264° |
| argument of perigee: | 188.9846° |
| revolutions per day: | 13.36121422 |
| mean anomaly at epoch: | 295.6229° |
| orbit number at epoch: | 89080 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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